# Service difficulty reports: N813ME, cancelled Aug 13, 2013

A list on [N813ME, cancelled Aug 13, 2013](https://openairdocs.org/deregistered/N813ME-2013-08-13.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 118 reports

- [SDR MWE2008F00025](https://openairdocs.org/sdr/MWE2008F00025.md): Lamp · inoperative · Jul 25, 2008 · N813ME · Doug DC981 · Emergency Lighting
  > RT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED RT OVERWING LIGHT. (K)
- [SDR MWEA080039](https://openairdocs.org/sdr/MWEA080039.md): Skin · dented · Mar 5, 2008 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE AT STATION 273 BETWEEN LONGERON 22 & 21 RIGHT. PERFORMED INSPECTION AT DENTED AREA, NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA080010](https://openairdocs.org/sdr/MWEA080010.md): Lanyard · failed · Jan 17, 2008 · N813ME · Doug DC981 · Escape Slide
  > DURING TAIL CONE SLIDE DEPLOY OPERATIONAL CHECK, THE TAIL CONE DROPPED AWAY CLEAN BUT THE SLIDE COVER DID NOT AUTOMATICALLY DEPLOY OR DEPLOY AND INFLATE EVACUATION SLIDE. REMOVED AND REPLACED TAIL CONE EVACUATION SLIDE.
- [SDR MWEA070308](https://openairdocs.org/sdr/MWEA070308.md): Spring · sticking · Dec 23, 2007 · N813ME · Doug DC981 · Leading Edge Devices
  > SLAT DISAGREE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. FOUND LEFT C SLAT SENSOR TARGET SPRING MECHANISM STICKY, CLEANED AND LUBED.
- [SDR MWEA070205](https://openairdocs.org/sdr/MWEA070205.md): Battery · discharged · Sep 6, 2007 · N813ME · Doug DC981 · Emergency Equipment
  > EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT 1A NOT SHOWING FLASHING RED CHARGE INDICATION. REMOVED AND REPLACED BATTERY.
- [SDR MWEA070202](https://openairdocs.org/sdr/MWEA070202.md): Panel · inoperative · Aug 30, 2007 · N813ME · Doug DC981 · Aerodynamic Fairings
  > TAIL CONE EXIT DOOR ARM/DISARM PANEL DOES NOT STAY IN DISARMED POSTION OR DOES NOT LATCH PROPERLY. RESECURED PANEL.
- [SDR MWEA070163](https://openairdocs.org/sdr/MWEA070163.md): Battery · inoperative · Jul 30, 2007 · N813ME · Doug DC981 · Emergency Equipment
  > AFT CABIN EMERGENCY FLASHLIGHT BATTERY INDICATOR DOES NOT FLASH. REMOVED AND REPLACED BATTERIES.
- [SDR MWEA070034](https://openairdocs.org/sdr/MWEA070034.md): Doubler · misdrilled · Feb 13, 2007 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > MISDRILLED HOLE AT STATION 180 JUST BELOW 2ND FASTENER FROM BOTTOM OF DOOR CUTOUT. PLUGGED WITH RIVET.
- [SDR MWEA070031](https://openairdocs.org/sdr/MWEA070031.md): Doubler · cracked · Feb 11, 2007 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > CRACK IN AFT LOWER AIRSTAIRS OPENING / FORWARD AIRSTAIR. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA060267](https://openairdocs.org/sdr/MWEA060267.md): Battery · inoperative · Sep 29, 2006 · N813ME · Doug DC981 · Emergency Equipment
  > ONE OF THE EMERGENCY FLASHLIGHTS AT THE FORWARD FLIGHT ATTENDANT STATION IS NOT TESTING. REMOVED AND REPLACED TOP EMERGENCY FLASHLIGHT BATTERY.
- [SDR MWEA060219](https://openairdocs.org/sdr/MWEA060219.md): Pressure Valve · inoperative · Sep 29, 2006 · N813ME · Doug DC981 · Cabin Pressure Control System
  > AIR CONDITIONING PACK WOULD NOT MAINTAIN THE CABIN AT FLIGHT LEVEL 20 THOUSAND FEET. REMOVED AND REPLACED PRESSURE REGULATOR VALVE.
- [SDR MWEA060218](https://openairdocs.org/sdr/MWEA060218.md): Wire · broken · Aug 7, 2006 · N813ME · Doug DC981 · Light System Wiring
  > TRACK LIGHTS AT ROW NR 10 INOPERATIVE. REPAIRED BROKEN WIRE.
- [SDR MWEA070017](https://openairdocs.org/sdr/MWEA070017.md): Flashlight · inoperative · Jul 16, 2006 · N813ME · Doug DC981 · Emergency Equipment
  > FORWARD FLIGHT ATTENDANT PORTABLE FLASHLIGHT STRAP BROKEN AND NOT CHARGING. REMOVED AND REPLACED FLASHLIGHT BATTERY & INSTALLED NEW STRAP.
- [SDR MWEA060136](https://openairdocs.org/sdr/MWEA060136.md): Oil Filter · clogged · Jun 24, 2006 · N813ME · Doug DC981 · Engine Oil Distribution (Airframe Furnished)
  > LEFT OIL STRAINER CLOGGING LIGHT ILLUMINATED. REMOVED AND REPLACED LEFT ENGINE MAIN OIL FILTER.
- [SDR MWEA060059](https://openairdocs.org/sdr/MWEA060059.md): Wedge · corroded · Jun 14, 2006 · N813ME · Doug DC981 · Ailerons
  > LEFT AILERON TRIM TAB INBOARD FILLER WEDGE IS CORRODED. FABRICATED AND INSTALLED WEDGE FILLER.
- [SDR MWEA060058](https://openairdocs.org/sdr/MWEA060058.md): Door Frame · corroded · Jun 14, 2006 · N813ME · Doug DC981 · Electrical/Electronic Compartment Doors
  > CORROSION ON ELECTRICAL ELECTRONIC DOOR FRAME STRUCTURE, LOCATED INSIDE THE ELECTRICAL ELECTRONIC BAY LEFT, STATION 218 LONGERON 28 LEFT. FABRICATED AND INSTALLED -T- CHORD SUPPORT ANGLE.
- [SDR MWEA060061](https://openairdocs.org/sdr/MWEA060061.md): Skin · dented · Jun 12, 2006 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED, TWO PLATES AT FRAME STATION 237 BETWEEN LONGERON 17 AND 18 LEFT. FABRICATED AND INSTALLED INTERNAL AND EXTERNAL DOUBLER.
- [SDR MWEA060057](https://openairdocs.org/sdr/MWEA060057.md): Attach Fitting · corroded · Jun 9, 2006 · N813ME · Doug DC981 · Leading Edge Devices
  > LEFT NR 2 LEADING EDGE SLAT, OUTBOARD ATTACH FITTING HAS CORROSION AT RETAINER SCREW HOLE. FABRICATED AND INSTALLED PLUG.
- [SDR MWEA060051](https://openairdocs.org/sdr/MWEA060051.md): Doubler · cracked · May 26, 2006 · N813ME · Doug DC981 · Leading Edge Devices
  > LEFT WING NR 2 SLAT OUTBOARD CENTER SLAT TRACK, APPROXIMATELY AT STATION XOS 240.0 EXISTING REPAIR DOUBLER CRACKED THROUGH 2 FASTENERS AND SKIN CRACKED PAST REPAIR TERMINATING AT PANEL 1136C, CUTOUT ON LOWER SKIN. FABRICATED AND INSTALLED DOUBLER AND FILLER.
- [SDR MWEA060050](https://openairdocs.org/sdr/MWEA060050.md): Support Angle · corroded · May 26, 2006 · N813ME · Doug DC981 · Fuselage Main, Bulkhead
  > CORROSION ON AFT PRESSURE BULKHEAD DOOR THRESHOLD SUPPORT ANGLE AT STATION 1338. FABRICATED AND INSTALLED SUPORT ANGLE AND SHIM.
- [SDR MWEA060049](https://openairdocs.org/sdr/MWEA060049.md): Frame · cracked · May 26, 2006 · N813ME · Doug DC981 · Aerodynamic Fairings
  > LOWER FUSELAGE FILLET FAIRING FRAME IS CRACKED, JUST FORWARD OF LEFT INBOARD FORWARD CORNER OF LEFT MAIN LANDING GEAR. FABRICATED AND INSTALLED DOUBLER AND STIFFENER.
- [SDR MWEA050032](https://openairdocs.org/sdr/MWEA050032.md): Doubler · cracked · Apr 14, 2005 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > SKIN CRACKED APPROXIMATELY 1.5 INCHES, PROGRESSING FROM FORWARD TO AFT SIDE OF RIVET, STATION 1380 ABOUT 1 INCH ABOVE LONGERON 14. REPAIRED DOUBLER.
- [SDR MWEA040195](https://openairdocs.org/sdr/MWEA040195.md): Bolt · missing · Oct 28, 2004 · N813ME · Doug DC981 · Fasteners
  > RIGHT MAIN GEAR UNSAFE AND AUTO SPOILER DO NOT USE LIGHT CAME ON. FOUND BOLT MISSING FROM RIGHT MAIN LANDING GEAR DOOR TARGET ALLOWING TARGET TO ROTATE AND PREVENTING DOOR LATCH FROM FULLY SEATING IN DOOR. REPLACED MISSING HARDWARE.
- [SDR MWEA040199](https://openairdocs.org/sdr/MWEA040199.md): Skin · dented · Oct 16, 2004 · N813ME · Doug DC981 · Passenger/Crew Doors
  > PASSENGER DOOR DENTED AND CRACKED. REPAIRED LOWER FORWARD CORNER DAMAGE WITH REPAIR DOUBLER.
- [SDR MWEA040155](https://openairdocs.org/sdr/MWEA040155.md): Finger Doubler · punctured · Aug 24, 2004 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > SMALL PUNCTURE IN FUSELAGE SKIN AT FRAME STATION 229 AND LONGERON 22 NEAR FORWARD LAVATORY SERVICE PANEL. CUT OUT DAMAGE AND INSTALLED FINGER DOUBLER AND PLUG.
- [SDR MWEA040090](https://openairdocs.org/sdr/MWEA040090.md): Attach Fitting · cracked · Jun 8, 2004 · N813ME · Doug DC981 · Fuselage Main, Attach Fittings
  > RIGHT MAIN LANDING GEAR DOOR ACTUATOR BULKHEAD ATTACH FITTING IS CRACKED. REMOVED AND REPLACED SUPPORT.
- [SDR MWEA040007](https://openairdocs.org/sdr/MWEA040007.md): Rivet · loose · Jan 10, 2004 · N813ME · Doug DC981 · Fasteners
  > LEFT AILERON SKIN HAS LOOSE RIVET IN TOP SKIN AT STATION XRS 475, HOLE IS ENLARGED. INSTALLED DOUBLER TO REPAIR HOLE IN AILERON SKIN.
- [SDR MWEA030275](https://openairdocs.org/sdr/MWEA030275.md): Pressure Switch · shorted · Jul 11, 2003 · N813ME · Doug DC981 · Landing Gear Brake System
  > AUTO BRAKE FAIL ANNUNCIATOR LIGHT ILLUMINATED AFTER PARKING BRAKE WAS RELEASED. REMOVED AND REPLACED SOLENOID PRESSURE SWITCH.
- [SDR MWEA030056](https://openairdocs.org/sdr/MWEA030056.md): Angle · cracked · Feb 5, 2003 · N813ME · Doug DC981 · Landing Gear Doors
  > RT MLG DOOR NR 1 FRAME TO INTERCOSTAL ATTACH T-ANGLE CRACKED IN THREE PLACES, LOCATED JUST OUTBOARD AFT OF ACTUATOR ATTACH FITTINGS. FABRICATED AND INSTALLED T-ANGLE, COMPLETED ALL REPAIRS AND CLOSED SKIN.
- [SDR MWEA030055](https://openairdocs.org/sdr/MWEA030055.md): Doubler · corroded · Feb 5, 2003 · N813ME · Doug DC981 · Trailing Edge Flaps
  > RIGHT OUTBOARD FLAP HAS MODERATE CORROSION ON INTERNAL SKIN SURFACE AND FRAME. -- REMOVED WEB AND CORRSION, FABRICATED AND INSTALLED WEB AND DOUBLER.
- [SDR MWEA030044](https://openairdocs.org/sdr/MWEA030044.md): Pulley · broken · Jan 24, 2003 · N813ME · Doug DC981 · Leading Edge Slat Control System
  > SLAT FOLLOW UP CABLE PULLEY IN THE SLAT SEQUENCE CONTROL MECHANISM HAS A SECTION BROKEN OFF. -- BLENDED DAMAGE.
- [SDR MWEA030030](https://openairdocs.org/sdr/MWEA030030.md): Skin · damaged · Jan 10, 2003 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > FORWARD CARGO DOOR OUTER SKIN IS DAMAGED ON THE LOWER EDGE NEAR THE CENTER OF THE DOOR. -- FABRICATED AND INSTALLED NEW DOUBLER AND SHIMS.
- [SDR MWEA030029](https://openairdocs.org/sdr/MWEA030029.md): Doubler · unwanted · Jan 10, 2003 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > REPAIR HOLE IN FUSELAGE SKIN WHERE EMERGENCY LOCATING TRANSMITTER WAS REMOVED. -- FABRICATED AND INSTALLED DOUBLER AND FINGER DOUBLER.
- [SDR MWEA03006](https://openairdocs.org/sdr/MWEA03006.md): Splice · corroded · Jan 8, 2003 · N813ME · Doug DC981 · Fuselage Main, Longeron/Stringer
  > LONGERON 30 AT STATION 593 IS CORRODED AROUND FASTENER HOLES THAT GO THROUGH THE SKIN. -- REMOVED CORROSION AND INSTALLED SPLICE.
- [SDR MWEA030015](https://openairdocs.org/sdr/MWEA030015.md): Web · damaged · Jan 7, 2003 · N813ME · Doug DC981 · Fuselage Miscellaneous Structure
  > FLOOR WEB OUTBOARD OF NR 1 SEAT TRACK AT FRAME STATION 313 HAS AN OBLONG HOLE. LOCATED AND DRILLED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA030014](https://openairdocs.org/sdr/MWEA030014.md): Skin · damaged · Jan 7, 2003 · N813ME · Doug DC981 · Fuselage Main, Longeron/Stringer
  > FORMERS AT STATION 237 BETWEEN LONGERONS 5 AND 4 LEFT AND 9 AND 8 LEFT REQUIRES REMOVAL TO FACILITATE SKIN REPAIR. -- LOCATED AND DRILLED NEW FORMER, FABRICATED AND INSTALLED SPLICE PLATE.
- [SDR MWEA030013](https://openairdocs.org/sdr/MWEA030013.md): Doubler · dented · Jan 7, 2003 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IS DENTED STATION 1250 BETWEEN LONGERONS 30 AND 29 LEFT. -- FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA030011](https://openairdocs.org/sdr/MWEA030011.md): Web · cracked · Jan 7, 2003 · N813ME · Doug DC981 · Fuselage Miscellaneous Structure
  > INTERCOSTAL WEB CRACKED BETWEEN LEFT FLOOR BEAM AT FRAME STATION 180. -- FABRICATED AND INSTALLED WEB.
- [SDR MWEA030010](https://openairdocs.org/sdr/MWEA030010.md): Doubler · cracked · Jan 7, 2003 · N813ME · Doug DC981 · Elevator Structure
  > RIGHT ELEVATOR OUTBOARD FAIRING UPPER ATTACH STRIP IS CRACKED. -- FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA030002](https://openairdocs.org/sdr/MWEA030002.md): Slat Track · damaged · Jan 7, 2003 · N813ME · Doug DC981 · Leading Edge Devices
  > LEFT HAND WING THE "O" SLAT INBOARD IDLER TRACK HAS A QUARTER INCH DIAMETER ATTACH HOLE THAT IS ELONGATED. FABRICATED AND INSTALLED BUSHINGS.
- [SDR MWEA030008](https://openairdocs.org/sdr/MWEA030008.md): Web · tool damage · Jan 7, 2003 · N813ME · Doug DC981 · Fuselage Miscellaneous Structure
  > REMOVED FRAME WEB AT FRAME STATION 1389 FROM LONGERON 30-24 LEFT TO FACILITATE OTHER MAINTENANCE. -- REMOVED WEB, FOUND SECTION HAS DOUBLE DRILL HOLES. -- FABRICATED AND INSTALLED NEW WEB.
- [SDR MWEA030007](https://openairdocs.org/sdr/MWEA030007.md): Intercostal · tool damage · Jan 7, 2003 · N813ME · Doug DC981 · Landing Gear Doors
  > RIGHT MAIN LANDING GEAR INTERCOSTAL BETWEEN STATION Y962.717 & Y970.343 AT X34.651 HAS A DEEP TOOL MARK. -- FABRICATED AND INSTALLED INTERCOSTAL.
- [SDR MWEA030005](https://openairdocs.org/sdr/MWEA030005.md): Skin · gouged · Jan 7, 2003 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > DEEP GOUGE ON INNER SKIN JUST AFT OF FRAME STATION 1485, RIGHT SIDE BELOW SMALL CATWALK STEP SUPPORT PANEL. -- FABRICATED AND INSTALLED REPAIR DOUBLER.
- [SDR MWEA030004](https://openairdocs.org/sdr/MWEA030004.md): Doubler · corroded · Jan 7, 2003 · N813ME · Doug DC981 · Landing Gear Doors
  > RIGHT MAIN LANDING GEAR DOOR HAS MODERATE CORROSION ALONG AFT EDGE. -- BLENDED OUT CORROSION DRILLED REMAINING HOLES IN REPAIR DOUBLERS AND INSTALLED FASTENERS.
- [SDR MWEA030003](https://openairdocs.org/sdr/MWEA030003.md): Intercostal · cracked · Jan 7, 2003 · N813ME · Doug DC981 · Fuselage Main, Longeron/Stringer
  > CRACKED INTERCOSTAL BETWEEN FRAMES Y958.117 AND Y962.717 14 INCHES OUTBOARD OF HINGE. -- FABRICATED AND INSTALLED INTERCOSTAL.
- [SDR MWEA020762](https://openairdocs.org/sdr/MWEA020762.md): Frame · corroded · Dec 27, 2002 · N813ME · Doug DC981 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT HAS MODERATE CORROSION ON TOP OF FRAME AT STATION 1322 LONGERON 29 RIGHT AND 26 RIGHT. -- REMOVED DAMAGED SECTION, LOCATED AND DRILLED AND INSTALLED NEW SECTION.
- [SDR MWEA020764](https://openairdocs.org/sdr/MWEA020764.md): Bushing · corroded · Dec 27, 2002 · N813ME · Doug DC981 · Leading Edge Slat Control System
  > RIGHT SLAT OUTBOARD SHEAR PIN SUPPORT HAS PITTING CORROSION IN THE BEARING HOLE. -- FABRICATED AND INSTALLED REPAIR BUSHING.
- [SDR MWEA020763](https://openairdocs.org/sdr/MWEA020763.md): Skin · dented · Dec 27, 2002 · N813ME · Doug DC981 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS SEVERAL DENTS STATION 238-245 BELOW LONGERON 6 LEFT. -- REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED NEW REPAIR SKIN.
- [SDR MWEA020759](https://openairdocs.org/sdr/MWEA020759.md): Longeron · corroded · Dec 26, 2002 · N813ME · Doug DC981 · Fuselage Main, Frame
  > FORWARD PIT BETWEEN LONGERON 30 AND LEFT 29 AT STATION 541 SKIN HAS MODERATE CORROSION. -- FABRICATED AND INSTALLED SKIN AND DOUBLER.
- [SDR MWEA020758](https://openairdocs.org/sdr/MWEA020758.md): Longeron · corroded · Dec 26, 2002 · N813ME · Doug DC981 · Fuselage Main, Frame
  > ELECTRICAL COMPARTMENT, FLOOR SUPPORT CORRODED AT FRAME STATION 220 BETWEEN LONGERON 29 RIGHT AND 30 ABOVE LONGERON 28 LEFT. -- LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT.

Next page: https://openairdocs.org/deregistered/N813ME-2013-08-13/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N813ME' AND deregistration_id = 'N813ME-2013-08-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N813ME-2013-08-13/reports

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